发明名称 Turbine airfoil with curved diffusion film cooling slot
摘要 An air cooled turbine airfoil with a leading edge region having rows of diffusion slots opening onto the airfoil surface. Each diffusion slot is connected to a plurality of metering and diffusion holes that meter the cooling air flow and provide for a first diffusion of the cooling air. The metering holes and diffusion holes are angled in order to improve the cooling effectiveness of the passages. The metering and diffusion holes and diffusion slots are formed from a metal printing process that can produce features that cannot be formed from an investment casting process that uses a ceramic core.
申请公布号 US8777571(B1) 申请公布日期 2014.07.15
申请号 US201113316485 申请日期 2011.12.10
申请人 Florida Turbine Technologies, Inc. 发明人 Liang George
分类号 F01D5/20 主分类号 F01D5/20
代理机构 代理人 Ryznic John
主权项 1. An air cooled turbine airfoil comprising: a leading edge region; a pressure side wall and a suction side wall extending from the leading edge region; a leading edge region impingement cavity; a row of metering and impingement holes opening into the leading edge region impingement cavity; a row of diffusion slots opening onto a surface of the leading edge region of the airfoil; a plurality of metering and diffusion holes connected to the leading edge region impingement cavity and opening into a diffusion slot; an axis of the metering hole is at an angle to an axis of the diffusion hole; the metering holes are angled in a radial downward direction; and, the diffusion holes are angled in a radial upward direction.
地址 Jupiter FL US